### lAW OFFICES OF WAYNE

## A. JOHNSON WAYNE A. JOHNSON, ATTORNEY 2901 W. PARKER ROAD#864434 PLANO,TEXAS75086 214.454.3292



### March 11, 2016 Docket ManagementFacility U.S. Department ofTransportation 1200 NewJersey Ave. SE West Building GroundFloor Room W12-140 Washington, DC 20590 Re: Drone Pilot, LLC ExemptionNo. 13801 Regulatory DocketNo. FAA-2015-2553 Dear Sir orMadam: - ' ' :..-' .; \ 

## ....

• j ._ • !,.(! \;**~-j;** 1j



### The FAA granted the request for exemption for Drone Pilot, LLC by letter ofDecember 1, 2015 as referenced above. Drone Pilot, LLC hereby applies for an amendment to the grant to (i) include the additional unmanned aircraft systems identified below, and 

### (ii) permitoperations for the additional purpose ofclosed-set motionpicture and television filming and production. The Unmanned Aircraft Systems. The unmanned aircraft systems (UAS) to be added (i) are lightweightrotorcrafts having a maximumtakeoffweight ofless than 55 pounds (including payload), (ii) will be operated at a speed ofno morethan 87 knots, (iii) 

### all contain built-in safety features, and (iv) are producedby UAS industry leaders. Proposed operations will be conducted under controlledconditions in airspace that is limited, predetermined, and access controlled. Operations will be subject to strict operating parameters to ensure at least an equivalent level ofsafety to currently authorized operations using manned aircraft. Petitionerproposes that itbe authorized by a grant ofexemptionto use any aircraft identified on the List ofApproved Unmanned Aerial Systems under Section 333 atregulatory docket FAA2007-3330 atwww.regulations.gov, when weighing less than 55 pow1ds including payload. Petitioner also proposes that it be authorized by grant ofexemption to use the DJI Phantom 4 and the RP Flight Systems Vigilant Cl (not currently on the list).**-~** --- 

### ljPage

### These UAS have commoncharacteristics. Each canbe operated by toggle or entirely by a touchscreen, map-based interface. This means the operator only needs to commandthe system where to go, and the system does all the flying for the operator. Theycanbe operated inboth semi and fully autonomous flight modes, with the operator simply clicking on a map to create a preplanned flight path for a flight. In addition, the operator can create no fly zones ormaximum flight ranges and altitudes so the system cannotenter areas deemed unsafe orunnecessary to fly over. In 

### addition, the UAS have built-in intelligent fault handling capabilities which allowthem to detect a system fault while in the air and automatically fly back to its take-offlocation and land. Faults that canbe detected include: loss ofcommunication; exceedingpre-set wind thresholds; and lowbattery levels. All flight operations are global positioning system (GPS) controlled, making the systems easy to navigate. At any point ifthe operator is not explicitly commandingthe rotorcraft systemto move, the system automatically holds its GPS position. The flight control system employs not only GPS positioning but a variety ofsensors including sonar, barometric pressure, temperature, wind speed andothers to ensure stability so long as windthresholds are not exceeded. All manufacturers maintain online product information portals with comprehensive downloadable operating and maintenance manuals, user guides, flight checklists, safety information and missionplanning instructions. Available also are instructional product and training videos along with robust online blogs andproduct forums. Information and specifications forthe DJI Phantom 4 canbe found at https://store.dji.com/phantom/phantom-4, and for the RP Flight Systems Vigilant Cl, seethe attached Appendix "A" RP Flight Systems manual. Standard Operating Procedures, Pre-flight checklists and Post-flight checklists were filed with the above-referenced application for exemption. Attached as Appendix "B" is the Motion Picture and Television Operations ManuaL
There has been no change in the conditions and reasons relativeto public interest and safety that were the basis for grantingthe original exemption. Thankyou.

Wayne A. Johnson

21Page

## Appendix "A" RP FLIGHT SYSTEMS MANUAL

31Page

# RPFLIGHT' SYSTEMS 

# INC.



# Spectra UA System User Manual**----------------------------------------------------------------------------------~**

RPFLIGHT SYSTEMS, INC. 

# Spectra MicroAirVehicle

# System User Manual

? RPF!ight Systems, Inc. P.O. Box 470 Wimberley, 1X78676 Phone: (512) 847-9746

# Table of

# Contents Introduction
...................................................................................1 Spectra Mission
............................................................................1 How to Use This Manual
..............................................................1 Spectra UA
................................................................................................ 1 Spectra Ground Control Station
.............................................................2 Technical Support
....................................................................................2 

## System Description
.......................................................................3 System Concept of Operations
.............................................................. 3 Spectra UA
................................................................................................3 Ground Control Station (GCS)
...............................................................3 Support Material
.......................................................................................4 

## System Operation
.........................................................................5 Ground Prep- GCS Power On and Software Startup
........................ 5 Flight Prep- Spectra Power Sequence
................................................ 6 Flight Planning- Map Waypoint Selection
......................................... 10 Drag and Drop
..................................................................................11 FOV Projection and Coordinate Reporting
.......................................... 14 

### Flight Sequencing
................................................................................... 15 Flight Sequence- Upload
.................................................................15 Flight Sequence- Fly
.......................................................................15 Flight Sequence -Loiter
...................................................................16 Flight Sequence -Land
....................................................................16 

### System Recharge- Spectra and GCS
............................................... 16 

## Operational Use Notes
.............................................................. 17 The GCS
...........................................................................**~**

### ...................... 17 Launching The UAV
...............................................................................24 

## Quick Start Checklist
................................................................. 26 UA Flight Planning and Modes
.................................................. 28 Troubleshooting
......................................................................... 29 Index
........................................................................................... 31REVISION -A 3/25/2007



# Introduction 

# T his manual presents a user with the infmmation needed to operate and support the Spectra Mkro Air Vehicle**~A)** system. The Spectra system includes two (2) Spectra air vehicles, one (1) Ground Control Station (GCS), one (1) carryingcase and assorted supportequipment. 

## Spectra Mission The Spectra UA mission is simple: AJlow a userin the field to gatherintelligence and "lookbehind the hill" withoutputtingthe user or any associates into harm's way. The Spectra conducts autonomous coYert surveillance flight while providing a live video feed totheuser.

ICON KEY Ji6 SpectrnAiocrafi: Ji6 Ground Control Station 2! Technical Support 

## How

# to UseThis Manual The "icon key" at left was shows three Icons that are used to indicate three different subjects in this manual. 111e first is the Spectra Aircraftitself, the secondis the Ground Control Station (GCS) used to control and receive information from the Spectra, and the last is impmtant technical details needed for general operation and support. Spectra UA The Spectra UA is a 

### 48 inch airframe, powered by Li-Po electric batteries and constructed out ofrugged impact resistant foam, ABS and carbon fibermaterial. Embedded in the foam are the important electronic components, including the Tiny Guidance Engine autopilot as well as communication modems and video camera and transmitter.. Future upgraded Spectras will combine these two transmitters into a single digit.al link. lnfo1mation specific to the aircraft is indicated in the document by the airplane symbol shown here.

1REVISION -A 3/25/2007 Spectra Ground Control Station :/' · The GCShardware consists ofa rugged tablet PCrunningWindows**~~~~··/** ; ;;;'/1; XP in conjunction with a set of hardware attached that includes

### '~-~ ... J '\: radio receivers, additional supportbatteries, shaker vibration motors**-~~.~-2~_;:,.~~.:-.::-=.** :...->.) and video to serial stream converterhardware. This system runs the CCD "Glass Cockpit" control panel software thatprovides mapping and video player supp01t, as well as command and control of the Spectra UA. Information on the GCS is indicated in the documentbythe computer symbol shown here. Technical Support ./ The technical support for the Spectra UA system includes battery chargers, spare parts for field repair and a rugged carrying case. Information on this hardware and otherinformation is indicated by the document symbol shown here.

2

## System Description System Concept ofOperations The Spectra UA system is shown below. The system includes two aircraft, a ground control station and supportequipment.

Spectra UA Minlawre UAV Eqwpoed**With~**

,, i\irrrl'lfi fJ"fl'l<;feiv("f • r•.1issirm Relay**Trnnscei~er** '' C:C[) V>f!fl(l Cft!ll<!fll • (;;Ps l{ucurvm

Figure 1.1SPECTRA SYSTEM Ruggoo {ln1egTale:tWt111 ' Tiltllet PC Ti:tf)ltll PC) ,**-~.' ~·** **·~-** ...**~~~-"~ ~L**  •• .., ..**-~** ..**~·** _ ..**...,_~-·**

A variant ofthe Spectra UA is shown below. The Spectra is an 18 inch flying wing with a pusher propeller power train. Embedded in the airframe core is the Tiny Guidance Engine autopilot with GPS, avideo camera, two Li -Pobatteries, a 900 :MHz datalink modem, and a 2.4GHz video transmitter. Also included in the airframe are servo motors for fin control and aDCmotor for propulsion.

Figure 1.2SPECTRA UA Ground Control Station (GCS) The typical GCS tablet PC hardware is shown below. Other tablets are used as the technology for battery life and daylight display readability progress., including the Panasonic Toughbook. Attached to the back of the GCS is additional support hardware including a 900 MHz datalink modem and a 2.4GHz video receiver for reception of the incoming video stream. A Video to USB converter provides digitization ofvideo stream for the user, and a vibrating alarm indicates to the userthe Spectra is approachingthe desired target.REVISION -A 3/25/2007

Support Material Figure 1.3SPECTRA GCS HARDWARE
The Spectra UA system also includes support equipment shown in the figure below. This support equipment includes but is not limited to a rugged carrying case, battery charger, andassorted field repair equipment (tape, propellers, etc.)

Figure 1.4SPECTRA SUPPORT EQUIPMENT

4ft!S Ground Control Station 

## System Operation The following list is a summary description ofoperating the Spectra UA System for video surveillance. Detailed information on each ofthe steps is described in depth laterinthis section 1. 

### Ground Prep

- GCS Power On and Software Startup 2. 

### FlightPrep

- Spectra PowerSequence 3. 

### FlightPJanning

- Map Waypoint Selection 4. 

### FlightConduct- Flight Initialization and Action
a. Upload- sends new set ofGPSwaypoints to the Spectra b. Fly -commands launch and fly outofthe Spectra to presetwaypoints
c. Loiter- selection ofthewaypointto loiter at d. Land-landinghierarchy 

### 5. VideoDisplayandMap OverJay 6. System Recharge Ground Prep- GCS PowerOn and Software Startup The GCS consists of an auxiliary communications box and the command PC. TI1e power sequence should be: ? TumPCpower on with aux comboxNOT connected ? Tumpower on aux combox 

### ? Plug USB cable from aux com box into tablet PC AFTER Windows has successfully booted, but BEFORE control software has been launched ? \"X/hen plugged 

### in, two familiar tones should be heard, indicating the video receiver and modemhave been initialized.MAll**A11i!ucl~** (m»llirne)

£S Ground Control Station REVISION -A 3/25/2007 

### ? Load the Glass Cockpit software A screenshot ofthe default Glass Cockpit screen is shown here:

Figure 2.1 CCD Glass Cockpit Software Instrumentation Screen V.deo**fe~d (r~!>l**  time)

This screen shows some key information aboutthe unit in flight, as well as theground control station. The Batterylevel indicator shows the GCS battery level and should be monitored so that theunit does not shut down due tolack ofpower. Once the GCS is powered on, the Spectra UA may be powered on. To prevent any potential startup problems, it is recommended thatpower to the Spectra occurAFIER the GCS control panel has been started. Flight Prep -Spectra Power Sequence TheSpecb:a UA is shown in the figure below. Thepropeller is held onby a propeller saver that allows the propeller to flex upon impact, preventing it from damaging the hardware uponlanding. Also shown are the attached side fins. Fins onboth right and left side are needed for launch and flight stal)ility. Flight ofthe unit is possible without fins, butnotrecommended -unstable flight will likely result and a crash will occur.

6REVISION -A 3/25/2007 Power on / offofthe unit is achieved by connecting the power connectors (male is battery, female is system).

Figure 2.2 Spectra UA The Spectra UA assembly occurs in the following steps: 1) Attach propeller (ensure clear ofdebris and free to rotate)
a. A correctlyinstalled propeller is shown here:

2) Attach fms
a. Fin attachment is shown here:

3) Power and initialization The Spectra UAis powered by connectingthe battery connectorto the rest ofthe system. This is shown in the figure below. Also shown in the figure are two cooling flaps for the motor controller. These prevent overheating ofthe system. Similarcoolingholes are located overthe video transmitter..

7REVISION -A 3/25/2007

Figure 2.3 Spectra PowerisApplied by Connecting Battery Connector (Male) to System (Female). Before connectingpower, the following conditions should exist ? The Spectra UA should be sitting on level ground after powerup, with the top of d1e wing facing the sky. ? A clear view ofthe sky is necessary for acquisition and tracking of satellites for GPS navigation. Failure toprovide aclear sky will result in inability to fly. ? The GCS should be kept a minimum oft foot away from the Spectrawhenpower is applied to prevent RF modem interference wid1 GPS operation and dan1age to the aircraftelectronics. After connecting power, the following secpence of events will take place. This 

### sequence of events can take 

### as long as 

### 15 seconds if 

### the GPS unit has 

### lost settings andmustbe re-initialized ? The Spectra UA will make an audible sound indicating the flight motor is ready. The GCS station will display 

### "TGEBOOTING"in the lower status message bar. ? TI1e Spectra UA will move the right control surface to indicate autopilot initialization is going to take place. It is 

### CRITICAL that after this initial servo wiggles the unitremain motionless until the next step. 

### IfVoice Notification is enabled, the system will announce to the user tohold the system steady. ? The Spectm UA will move the left servo indicating that the unit initialization is complete and GPS acquisition has begun. This typically takes less than 1 /2 second from d1e first elevon movement. TI1e GCS station will display 

### ''RUNNING" in the lower status message bar. On the l'vfAP and GPS pages, the mode displayed will indicate 

### "INIT". 

# •REVISION -A 3/25/2007

o If no messages are received and the control surfaces do not move within 15 to 20 seconds, it is likely that there is a communication failure in the uplink to the plane. Power down the plane, and attempt again. Ifunsuccessful, power down the plane and system and repeat the ground station initialization (close the Glass Cockpit software, unplugthe aux com box,waituntil audible disconnectis heard, repeat plugin / startup ofcom box and Glass Cockpit software). ? Between 10 seconds and 1 minute after this message, the mode indicator will transition to 

### ''LAUNCH READY", indicating that there are sufficient satellites for a solution fix.
o This time is directly driven by GPS satellite visibility. The GPS tab shows progress and satellite tracking.
o IF NO POSITION IS ACQUIRED after 1 minutes, it is likely that there is some interference or other jamming preventing GPS acquisition. The system shouldbe movedto a different location that has a clear view ofthe sky andno obstructions to allow acquisition.


### o THE UNIT WILL NOT ALLOW LAUNCH UNLESS THERE IS A GPS ACQUISTION AND SOLUTION! A minimum of4 satellites mustbe in track to allowflight ? If a video transmitter switch 

### is included in the Spectra unit, it 

### is recommended that this be in the OFF position until launch 

### is ready. This will prevent possible overheat / brown out ofthe video transmitter due to lackofairflow cooling.



# ... ...

.

# .. 

# • 

# ,. 0 

# ..

Figure 2A V"Jdeo Transmitter On I Offswitch : 0 

## = on, I

## = Off

9REVISION -A 3/25/2007

Cl**Qual~t.y** : o C2**·~ual~t.y** : 0

Cll QualH,y : o C12 •::!uality : 0 C13**Qual~ty** : o C14 •2uality : 0 C15**•:!ual~ty** : 0 Cll CNO : 0 C12 CNO : 0 C13 CNO : 0 0.:14 CNO : 0 0.:15 CNO : 0

Figure 2.5 GPSStatus Screen Shows 7 Satelites in SolutionofVarying Strength. Mode shows Spectra is ready for Launch.
Flight Planning - Map WaypointSelection While the system is acquiring satellites for GPS navigation, the GCS map set can be used to enterup to 8 waypoints into the system. Upload ofwaypoints should occur only afterthe unit has finished initializing. Shownbelowis the Map tab screen

10Header information --- Highlighted waypoint information

Flight Plan commands: Upload Loiter (now) Land (now) Fly Abort Resume REVISION -A 3/25/2007

Drag and Drop Figure 2.6Spectra GCS Flight Planning MapScreen The map screen supports drag and drop / point and click functionality. Clicking on a section ofthe map and dragging it will scroll the unit, and clicking onwaypoints will showthe defmed actions to be taken at thosepoints. The function keys atthebottom ofthe map represent capabilities specific to the map. A description is shown in the figure below.

11NewWaypoint Delete Current Waypoint REVISION -A 3/25/2007

Select Map Directory and settings Currentwaypoint properties

I Save 1 Zoom in J Load . out waypo1nt files action current waypoints I

Figure 2.7 Spectra Map Functions The map functions have the following properties: 

### MAV Start new waypointfile

? Add 

### I Delete Waypoint- Add will place a newwaypoint in the center ofthe currentmap screen. Delete will delete the currentlyhighlighted waypoint. ? Undo 

### I Redo- Selfexplanatory ? Save 

### I Load Waypoint ftle- .wpt ftles can be created or uploaded that have storedwaypoint ftles for the system ? Zoom 

### (+I-) -willzoomthe map in and outwithin range ? GOTO- Sets mappingfunctions and data paths (described later) ? Goto**~xt** Waypoint

- This button will highlight and zoom to the next waypoint in the sequence. It is only for ease in navigatingthe map screen, and has no affect on the aircraft ? See All Waypoints

- This button will scale the map to include all current waypoints As indicated, tl1e GOTO button enables the following setup screen for map data and contour scaling

12REVISION -A 3/25/2007

...7;c:l
...., Go To location
.. ···" • . ·,., rOataSource**-~-** Path: 

# I• Format: 

# I CADRG DTED Path: IC:\code\ccdpanei\Release\ma1**~** Load

r-Loaded Map Info ------------------- CA.DRG format
.... 2221 frames inA.TOC Rough Latitude extents: N 18 deg 51.172 min· N 42 deg 3.384 min Rough Longitude extents: W 160 deg 35.465 min· W 117 deg 5.482 min DTED format 167 frames loaded 

## ..:J
Cancel IDTED settings ---·---- 

## -"-! 

# I Minimum Elevation r.: 

### 10

:------::u':"'1. 1 (Blue level): ...::.J ! I Maximum Elevation (Red level): 

## j6oo
I 

### P Color Map Based on Elevation 

## I Set
____

# _j

rLocation --- -----··----- 

### I 

# ! Map Series: j1 :50K j Latitude:j**~N~33~d~e-g~3~5~.0~2--5-m-in** ____ _ Longitude: 

## jw 117 deg 45.715 min MGRS: 111SMT2929716265 Go World View Figure 2.8 GOTO MapAdjusbnent Screen The GOTO Map Adjustment screen contains four frames. 1be frames contain the following informationand actions: 

### ? Data Source
o Path: Path to the CADRG data set to be used for flight operations. Typically, a CD of CADRG map data for a selected region will be loaded onto the GCS. This path indicates where t11at data is stored.
o Fonnat: CADRG or imagery data (an advanced option if satellite in1agery is available)
o DTED Patl1: Path to the DTED elevation data set to be used for flight operations. Typically, a CD ofDTED map data for a selected region will be loaded onto the GCS. This path indicates where that datais stored. DTED Ievell is recommended. 

### ? Loaded Map Info

13REVISION -A 3/25/2007 .·'

o A summary ofthe loaded map data based on the paths in the ''Data Source" section. 

### ? DTEDSettings
o Used for scaling of the colors applied to the maps, the minimum elevation (in meters) and maximum elevation are entered here for visual cues to elevation if the DTED data is available. This is an option, and ifnot desired the "Color Map on Elevation" box should be left unchecked. 

### ? Location
o TI1e currentmap series (CADRG defined), as well as the currentview Latitude, Longitude and MGRS coordinates are shown. Typing new coordinates into this location and hitting "GO" will reset the view of the map screen. FOV Projection and Coordinate Reporting Shown onthe map screen below are a number ofimportant features. A description of each follov,-s: 

### ? AircraftInformation: This banner shows current aircraftposition, altitude, and heading information. The current flight mode 0nitialization, launch, flight, loiter, land) is shown, as well as an ETA and distance remaining to the next waypoint. 

### ? Cursor Information: Hovering the cursor over the map provides latitude, longitude, altitude (ifDTED data is provided or available) as well as MGRS coordinates. 

### ? Command Buttons: 'TI1ese buttons are used for deftning the commanded mode ofthe system and are described later in this document. 

### ? Status Messages: These messages provide the userwith information regarding the airvehicle health and operation. 

### ? FOV projection: TI1is red outline indicates tl1e video camera field ofview, and can be used to determine where tl1e aircraft video camerais currentlylooking.

14REVISION -A 3/25/2007**ttd:tr~JJlL~p)~ a::wtfi-;-~~-=;-~-lb~~-:~J** **~~:U;;~£-:::u-·** 

### -- Instruments! Relds**~Vide**of Config jMemoryl User DBIB

# l Graphs

# I**Raw[~P'** GPS 

## I



# .. --------**-~-** N "'3 deg 4<:**.~s** -mifl sa ft 15 cteg. ' ' ' • 111 117 deg 55.305 l'l>1n :" , , HSHT14Se329B2o

- No Hessages Received**-~5Hz ----~-·--**  :1 StatusMessages**----~1** FOV Projection Command Buttons
Figure 2.9 FOV Projection and Coordinate Reporting Flight Sequencing IAircraft coordinates, caltitude and heading, 

# l ':aswell as mode, ETA and distance to next waypoint Cursor Lat/Long/Ait Height and MGRS

! Function Keys

The followinglist describes the modes ofoperation forthe Spectra UA System Flight Sequence- Upload This buttonwill upload the current set of8 waypoints to the Spectra UA. The current set ofwaypoints storedin the UAwill be ovetwrittenwith the new set. Flight Sequence- Fly This buttonwill commandthe Spectra to enter flight mode. Provided a GPS lockhas been achieved, the Spectra will begin to look for indication that the user has hand launched the unit. W'hen thrown with enough speed, the propeller will start to turn andthe unitwill climb to altitude.

15REVISION -A 3/25/2007 Flight Sequence- Loiter Tins button will command that the current highlighted waypoint be used as the loiter pointfor the unitifdesired. Ifno loiterpointis entered, the Spectra will proceed along the designatedwaypointpath from launchtoland. Flight Sequence- Land This buttonwill force the unitto cutpower andland immediately. System Recharge- Spectra and GCS The Spectra UA contains two, kell Lithium Polymer batteries with a 2100 mAhr capability each. The system should be charged with a L-Po charger that is set for charging a 3-cell, 11.1V battery set to a 4,200 mAhr capability. This would allow a 2 amp charge capabilityifusing aThunderPoweror equivalent charger. The Auxiliary Communications Box contains a single 2100 mAhr, 3-cell, 11.1V battety. There is no battery indicator onthe aux com box. It should be recharged after 1 hour ofuse. The GCS should be charged using it's AC power adapter if possible. The GCS contains aLi-Po battery as well, buthas more capacity and could be damaged by failed charging capability. From depletion, a full charge may take as long as 4 hours for the GCSsystem.

16

## Operational Use Notes TI1e actual operation ofthe system requires time in service to be most effective. This section contains notes from the development and prototype testing that should help otherusers fly the Spectra system. TheGCS The Ground Control station is a rugged tablet with USB connected communication devices ontheback 

### Do notdisconnectthe USB cables during operation, as you 

### willlose communicationwith the UAVand potentially lose the UAV itself. There are six (6) maintabs ofinteresthere. Each is described briefly below. 

### COCKPIT The Cockpit screen shows the artificial horizon and battety voltages ofinterest. Pib.is screen is useful for determininggeneral system health.!5 : 3 REVISION -A 3/25/2007

F!1ght l!ode : 0 TI>rottle : -1.0000



### VIDEO The video tab displays the 640 x 480 video stream in real time. This is the la1gest display ofvideo in 

### the control panel. Located on the left are the last three projected locations d1at are logged when the user double clicks on the video image. These locations are presented on the map page as flags. Ifno video is present (indicating a GCS system failure), then the display "No Vireo" will

### be shown.

18REVISION -A 312512007



### S/WSetup [00:22)



### This screen allows setup ofRF power on the aircraft as well as local settings on the ground station (like communication channeQ. Besides the communication port number, which may change depending onportplugged into the system, none ofthese settings should be changed. They are for advanced users and experimentation applications. 'The following settings may be changed: Listen Only

- If

### you want to use the system as a duplicate and to only view data coming from the UAV, clickthis icon. When activated, nocommand and control will occurfrom this unit. ACK

- Used for the deadman switch on the UAV. 

### For prototype testing, the deadman capability will make the plane return to home Qaunch point) if communicationwith the ground station is lost. :MISC Options- EnableVibration Alert-This enables 

### I disables the motorvibrator. :MISC Options

- Voice Notification

- This enables 

### I disables audible voice notifications ofsystem state.

19REVISION -A 3/25/2007

1G: C••flllt**:co~G.** 

### :::J

e,.,dl-1<1•**r;:.~~~t~:l-~......;:3, li.,.;.,nT~** **(0·~•** 

### :::J

# ~~I I ""-L•.-.1 jsooum 

### .:::J 11r**A,~, tn~n·lti>>**  

### :::J r; olD'. 

### r**~·**

### o,. .,
florVIollmbooQ::.ri.J**.o~.u...** 

### r. 

### l 

# I I FIFFliO< 

### J,..-----3'"1 

## '""""Mi
... I W'lJ•flFA•., 

### F"""'l""" 

### i 

### 3**ihlt<~•f'.:.o"**

(.....tlo>''"""AJ.ol**~V"'::CJU:.tU~:** 

# =**S'iMu¥;~iWtl =lllR.,Ff~l** 

.usa 

# """''**V.o~i~Ptc.l't&W't** CllrhdP..,.I**(10.~21** 1EFI"""'" joo

r.• .:r.·a·( •. -.**~-r** ·"·**-~-r** (CO J•] 

### COMMAND This tab provides access to anumber ofadditional commands. Importantcommands include: Re·lnit 

### Gyros -Ifthe system was powered while being handled, or the rates shown indicate that the rate sensors were improperly initialized, set the unit down in a motionless position and dick on this item. TI1e gyros will be reset to 

### a known zero value. Come Home

- System will be commanded to return to the launch point This command is useful to force the unit to return to the user no matter where it is in the flight path. Throttle 

### ++ / - : Ths allows modification of the throttle on the plane. The reduction(--) is particularly useful for landing the plane gradually. A COME HOl\ffi command will make the plane return to the user, and as it approaches multiple THROTTLE- commands will decrease it's altitude and allow closer landing. IT IS IMPORTANf 1HATYOU «ABORT'' or «LAND**~OW''** 

### the system before it hits the ground to make sure there is no damage tothe system.
20REVISION -A 3/25/2007 

### Center Servos On (and Oft) turns motor off and centers servos for optimum storage configuration. Use this before powering down the system to stow it in the carrying case. Tum it offifthis was accidenta11y engaged and you want the unitto fly. 

### IMPORTANT-Do NotTurnThis OnDuringFlight- Planewill 

### crash!! Deadman Toggle enables 

### I disables the deadman function. If enabled (default) and the UA does nothear from the ground station for 20 seconds, the Spectra UAwill enter «Come Home" mode. If, after another 40 seconds, no ground communication bas been heard, the system will go into a ''Land Now" mode. Disable this function iflongdistance 

### (> 1km) flights are intended or ifthe GCS may notbe aJlowed to transmit an acknowledge tothe aircraft.

# ~**~~--** . 

## .. .. .


# .**~** 

### :o2.021 GRAPHS This tab displays real-time sensor data and can be important to check caJibration. If the accelerometers do not record a 

## +I-1 when oriented with the ground, the accelerometers should be recalibrated. Ifthe magnetometer va1ues exceed 

### +

## 1-1 then the magnetometers shouldbe recaJibrated. Contact CCD for recalibration procedures.

21REVISION -A 3/25/2007



### MAPSAlready described in this manual, path planning, launch, Loiter Now, Land Now, and Abort/ Resume commands are active here as well as onthe CommandTab.

22REVISION -A 3/25/2007

I)

P.laY.B c o er1 lAUNCH Command

### Rece~ved- .

### ~I001IDQJ\tli:llml : 

### .**~** - .,_.- - .,'

111is is a critical tab. It provides the user with infotmation regarding GPS lock. Without lock, there cannotbe any flight.

23REVISION -A 3/25/2007

C13 Qualit.y : 0 C14 Quallty : 0 C13 •:NO : 0 C14 CNO : 0 C15 Quallty : 0 C15 CNO : 0**~** L,;,UIK H (_.'C,I(ilnano:l I=":.:>U'I·1'?'1 [00:06)**--------------------~** Launching The UAV 111e sequence for flight is as follows: ? Powersystem on ? Verifv attitude and healtl1 ? Upload waypoints ? Command launch ? 1l1rowaircraft intowind, at aclear segmentofsky (i.e. notrees ifpossible) 1ne unit will hold the heading when launch is detected by a 4G tl1row. It is IMPORT ANTiliatyou throw the plane level and straight. Theheadingis locked in at launch, and ifilie arm is cocked orthere is oilierinterference on launch, itcould affect flight. Shown here are the suggested orientations for launch (using an older pusher propellerversion ofthe Spectra UA).

24REVISION -A 3/25/2007 Note thatthe wing should be pointedup at approximately 30 degrees. The unit should be thrownlike a dart, shown here:



### Do NOT throw the unitlike a baseball, cockingyourwrist, as shownbelow. It will lock in 

### a 45 degree or more offset on launch thatwill like cause a loss of altitude onlaunch, possibly

### hitting the ground.

25

## Quick Start Checklist The following list should be used for simplified flight operations. 

### ? Turn on GCS and ensure that auxiliary hardware is powered and attached via USBcable(s). 

### ? Startup Glass Cockpit software:
o Verify red TX indicator in bottom left corner is blinking once per second (datalink is active when this is true)
o Verify "NoVideo"is NOT displayed onvideo screen (video reception is active when this is true) ? Place Spectra UA on level ground Do not hold in hand, and do not allow wind to be movingplane for initialization. 

### ? Connectpowerwires for Spectra UA andleave undisturbed ? Verify status messages indicate ''TGE Booting"within 5 seconds ofpower on IfVoice Notification optionis turned on,unitwill audibly indicatebootingand other messages. 

### ?**\~fait** for initial right elevon wiggle, then left wiggle, making sure unit is motionless duringthis time. Donothold in hand duringthis time, and do not let wind gusts move plane. After wiggles are complete, you may move the plane as you would normally. Do not shade unit from acquiring satellites for GPS navigation. ? Once a GPS lock is achieved, the Spectra UA will appear on the map screen. Verify waypoints for mission are entered correctly and choose UPLOAD on the map page to reprogramSpectra UA 

### ? Click on FLY when reported MODE on map screen indicates 'Launch Ready"
o IF "GPS LOCK LOST' message appears after launch command is received, unit has lost lock and 

### WILL NEED TO BEREVISION -A 3/25/2007 

### COMMANDED THROWING! TO LAUNCH AGAIN BEFORE
? Throw Spectra straight and with speed and at a pitch angle of 30 degrees towards a clear flight path (no obstructions, etc.) 

### ? Spectra will fly in the direction of the lannch until 60 feet above the launch altitude. Itwill then proceed to first waypoint location and altitude. ? Depending on path planning, Spectra will either Loiter at designated position or fly to each successivewaypoint. Ifthe last waypoint is reached and itis not designated as a LAND waypoint, the path will continue with the first waypoint. 

### ? Buzzer will sonnd and vibrate within an estimated 30 seconds ofapproaching the nextwaypoint. 

### IT IS HIGHLY RECOMMENDED TO DISABLE THIS BUZZER ON THE S/W SETUP PAGE TO SAVE POWER ONTHEGCS. ? ViewMap andVideo screens to receive intelligence on activitywithin FOV.
o Clicking onthe video image will drop a flag onthe map indicatingthe point of interest. A buffer of three (3) points of interest will be updatedin a first in

- first out manner. ? Click on "LAND" ifunit should land immediately. Click on ''LOITER" if a Loiter is desired at the currentposition. Click on ''RESUME"tobreak loiter. Click on "ABORT" to shut the motor off and glide to the ground immediately. ? Last waypoint will be default to be alanding point for nnit in lieu ofLAND command Ifthis waypointis turned to "CONTINUE",the UAV will fly thru all waypoints repetitively.

27REVISION -A 3/25/2007



## UA Flight Planning and Modes The Spectra UAperforms the following actions in different aspects ofit's flight modes: ? 

### INIT -NoGPS lockhas been achieved, flight will notbe allowed. Waypoint planning and upload is allowed however. ? 

### LAUNCH READY- GPS Lock has been achieved. Ifa ''Launch" or "Fly" command is received, the unit will wait for a hard throw to proceed to the 

### CUMB mode. When the hard throw is detected, the current heading is locked into memory before proceeding to the climb mode. If, during this mode, GPS is interrupted, then a "GPS Lock Lost" message will be received, and any "Launch" or "Fly'' command previously sent will have to be resent onceLaunchReadymode is entered again. ? 

### CUMB

- In this mode, the heading sensed on launch is held and the unit tries to achieve altitude ofthe first waypoint. This modewill be activeuntil the following criteria are met
o Ifthe GPS measurement indicates that the UA is 20 meters (-60 feet) above the law1eh point, then d1e unit will transition to

### WAYPOINTS mode
o If, after 20 seconds, the UA has not achieved altitude of20 meters, it will tum 

### 180 degrees around and continue totryfor altitude.
o If, after 40 seconds, the UA has not achieved altitude of 20 meters above launch, the motor will shut down. It is assumed that there is somethingwrongwiththe UA mechanics.
o 1 second after launch, another 4 G shock to the system will tum the motoroffas well. This is a safety feature. 

### ? 

### WAYPOINTS- This is the notmal flight mode. In this mode, the buzzer will be active and vibrate when the ETA is less than 30 seconds. ? 

### LOITER- In this mode, the system is loitering about a waypoint or about a commandedposition.

28

## Troubleshooting Primary issues encountered are as follows: ? No Red "TX"light orcommunicationwith plane
o GCS system may nothave bootedproperly. Follow the steps below: J!S Shut down 

### all programs andpowerUA dov.n. J!S Disconnect USB cables from Tablet. Wait for audible indication ofdisconnect. J!S Reconnect andwait for audible indication ofreconnect J!S Open XCTU program to see list of available serial ports Qooking for USB to Serialp01tin particular). J!S CloseX-CTUprogram and open Glass Cockpit. 2S On SIW setup page, make sure thatthe comportis the same as that specified by X-CTU. Also, verify that "ACK" is checked and ''Listen Only''is unchecked. 2S Hit''RECONf\lECT'' and red 

### ''TX" light shouldbegin. ? No map datais shown
o Verify map data file is for the area where system is beingused
o Use the "GOTO"button onthe map page to setup map data entries
o Wait for GPS lock from UA, thenhitthe Plane buttonto zoom tothe location ofthe actual plane. Zoom in tothe correct scale for the map data beingused. ? Plane did notturnpropelleronwhen I threwit
o Launch command not sent 

### I received

- verify via status message 

### I voice notification thatthe launch commandwas received.

29

### o The GPS never achieved lock- verify lockbefore throw
o The GPS lost lock after the launch command was received -tum audible notification on to warn oflostlockbefore throwingplane.

30battery, 2, 5, 7, 8, 9, 18, 19 CADRG, 15, 16 DTED, 15, 16 FOV, 16, 17 GCS, 1, 2, 4, 6, 7, 10, 12, 13, 15, 18, 19, 29, 30, 32 Glass Cockpit, 2, 7 GPS, 3, 6, 10, 11, 12, 17, 25, 29, 31, 32, 33

31 launch, 6, 7, 16, 18, 21, 22, 24, 26, 27, 29, 31, 33 Spectra UA. 0, 1, 2, 3, 4, 6, 7, 9, 10, 17 MGRS, 16 servo, 3, 10 Tiny Guidance Engine, 1, 3 Waypoint, 6, 12, 14P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746 

# SPECTRA Fie I 

# d Manua I 

# Three Camera Module

Continued
All Content & Images Copyright© RPF!ightSystems, Inc. I /P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746 RPFlight Systems Spectra is shipped in its carrying case as shown below. Take the time to look overthe contents before removing items so that you can easily return them for transp01t later.
. Familiarize yourselfwith each ofthe items and thenomenclature used for each. The more familiar you are witheach component makes this field manual easier to use. All components will be identified in this manual and with representative pictures ofeach. Some images may not look exactly like your platfonn, but the focus ofthe image will be described in the text to help clarify it's use.

1. Ground Control Unit 7. 12V Lithium video battery 2. Lumix DMGLX2 Digital Camera 8. Lumix Software and Manual 3. Yellowjacket Diversity Video Receiver/Antenna 9. Lithium charger 4. Lumix Battery Charger 10. Spectra Flying Wing 5. 12V 4200 mah Lithium Polymer Flight Packs 11. Parts/Tool Kit 6. Ground Contwl Charger 12. Spare Propellers
Continued All Content & Images Copyright© RPFlightSystems, Inc. /m· /t!J, 

# ,c, " 

# ..P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746
The onepiece Spectra flying wing is a greatly simplified version ofthe original three piece modular design. The equipment is cradledin foam and is well protected. Itis very easy to gain access to the main payload area ofthe Spectra, exposing the digital camera, flight pack,videopack as well as other flight electronics. 

# I 

# ·J&:.·
......

·._.)

.: . ., I <-Removethe 1/4-20 nylon screwholdingthe top fairing.

With the aircraft facing --"., ( towards you, carefully rotate 

### Ill,/ the top to the left side ofthe aircraft as shown
. 

# Payload Area Components

I. Outrunner Electric Motor 6. Camera Shutter Servo 2. GPS Unit 7. Flight Control Receiver 3. On Screen Display Elecb:onics (OSD) 8. MainFlight Pack Power Plug 4. Video system powerplug 9. Thermal Stabilization Switches 5. Lumix Camera Cradle 10. Thermopileribbon cable Continued All Content & Images Copyright© RPF!ightSystems, Inc.P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746 

## Adding the payload components The most typical requirement for your Spectra will be for the collection ofhigh resolution digital imagery. The Lumix included with 

### your flight kit is a very capable imager and will take excellent pictures from all altitudes. Wehave found the best results are produced by using the following settings: Make sure the proper aspect ratio is selected on the barrel ofthe lens. 16:9 gives the widest angle available.
Afterpowerup the Lumix, make sure the function dial on top is setto "SCN"or SCENE.



## I 

# (:::J The screenwill display several

-1 available SCENE possibilities. Select the "SPORTS"mode. This gives the highest shutter speed possible.
Place the camera in the cradleand ensure the shutter servo arm will contactthe shutter button.
We highly encourage the user to explore the other settings on the camera and experiment with what works best in the conditions most likely encountered. There are other settings thatwe have found effective and they are as follows: 1. We have learned that setting the autofocusmode to MANUAL and settingthe focus oninfinity speeds up the time it takes to take a picture. 2. Setting the Optical Image Stabilizationmodeto "NONE" or "OFF" actually helps to sha1pen images. 3. Ifimages are going to displayed on a standard TV screen set the aspectrationto 4:3. 4. Using fast SD cards shortens the time between shots. 5. Ifyou are required to waitbefore launch, be sure to shoot one shot every 10 minutes to keep the camera from going into sleep mode.



# Continued
Al1 Content & Images Copyright © RPFlightSystems, Inc.P.O. Box 470 Wimberley, TX78676 Phone: 512.847.9746 

## Preparing for flight operations WARNING! Do NOT plug in the main flight pack batteries unless the ground control station is turned on and tuned to the correct frequency! Doing so could place the operator and bystanders in risk should the motor start unexpectedly!**~** Ensure that the ground control unit 

## V is on the correct frequency for the aircraft you intend to fly.

After powerup ofthe GCU, ensure the correctmodel is displayed on the GCUscreen
.

. Once the GCU is powered up, connectthe main flight pack as shown. Try to connect it smoothly without multi contacts ofthe connector.

Place the main flight pack into the nose ofthe aircraftas shown
.. When connected, ensure that all bystanders are clear ofthe propeller in case ofradio interference
.

...,..,.---.... Ifthe digital imager is to be used, test the shutter control nowtoensure 

# Continued
All Content & Images Copyright© RPFiightSystems, Inc.P.O. Box 470 Wimberley, TX 78676 Phone: 512.847.9746 

## Preparing for flight operations Ifthe live video feed is to be used, locate and plug in the small 12V lithium polymer battery to the correct plug in llie aircraft.

The video battery pack is placed behind the digital image carrier as

### T===:::======~==~~shown.

## ~====~~====::!_ Locate the correct winglet and insert the pins into llie sockets, securing the winglet to the wing

The winglets should fit snugly against the wing tip as shown

After ensuring lliat all flight controls are functional, replace the pod top on the airframe and secure withthe 1/4-200 nylon bolt.

After flight preparation and before launch, keep aircraft away from by**Lr::=~======~~~::::==:::J** standers and support personnel.


# Continued

All Content & Images Copyright© RPFlightSystems, Inc.**r~'** I

## Field Pre-Flight Checklist Print and laminate this checklist for field use before every launch!

1. Check voltage onbatteries/systems to beused 2. Tumon, and insert imager inpayloadbay 3. Plug in videobattery (ifused) 4. Ensure proper frequency ofground control unit (GCU) 5. Tumonground control unit (GCU) 6. Verify correctmodel is selected on GCU screen 7. Announce "GCUpowerup andready!" 8. Plug inmainflight pack and insert in airframe 9. Announce "Airframe armed!" I0. Check function ofimager/payload servo 11. Re-assemble pod top withnylon screw 12. Verify video signal is available and transmitting (ifused) 13. Ensure on screen display (OSD) is functional Flight Control Check 1. Check for correct elevonmovement UP-Pull back on right GCU stick, elevons shouldmoveUP. 2. Check for correctelevonmovementDOWN-Pushforward onright GCU stick, elevons should move DOWN 3. Check for correct elevon movementLEFT-Move right stick GCU stick tothe left. Leftelevon should move up and rightelevon should move down (as viewed from the rear) 4. Check for correct elevonmovement RIGHT-Move right stick GCU stick to the RIGHT. The right elevon should move up and left elevon shouldmove down (as viewed from the rear) 5. Announce "Standclear ofprop!'' andmove the left GCU stick forward to ensure correct rotation ofpropeller. 6. Announce "Ready to launch" and move totheplanned takeoffzone. 

### Flight Safety Procedures 1. Review primary launch and landing site with all personnel before launch. 2. Plan for the shortest possible flight time unless the mission calls for extended orbit ofvideo feed. 3. Designate observer(s) for each and every flight. 4. Do not allow personnel not directly associated with the mission to talk 

### to the pilot in control. 5. Plan a contingency landing site for hazardous nnss1ons. 6. 

### In NIMS structured incidents, do not launch withoutprior approval ofthe Incident Commanderor incident designated "airboss". 7. Pilot should announce "Launching!" so that all personnel involved can hear. 8. Pilot should announce "Landing!" so that all personnel involved can hear. 9. Observer(s) should fall back to the landing site (ifpossible) and act as safety personnel to keep landing site clear during final approach. 10. Pilot should announce "Aircraft secure!" and advise IC or incident "airboss" thatthe aircraft is down and secured.



# Continued
All Content & Images Copyright© RPFiightSystems, Inc.P.O. Box470 Wimberley, TX 78676 Phone: 512.847.9746

Air Crew Designations-Current FAA descriptions as ofAugust 2008 Pilot in Command (PIC)-This person is primarily responsible for mission planning and overall operation ofthe mission. Pilot in Command will take into consideration any and all operating procedures as set forth by the agency requesting the mission. Pilot At Controls (PAC)

- This individual is primarily responsible for the safe operation ofthe aircraft, and to execute the mission as set forth by the Pilot In Command). The Pilot in Command and the Pilot At Controls may be the same person in some circumstances. Observer-Thisposition is to act as a back up and assistant to the PilotAt Controls. This person will observe the aircraft dwing its' mission and will also advise the PAC iffull scale aviation assets should enter into the mission area. Seconda1ily, this person will act as a safety officer during takeoffs and landings. The Obse1ver MAY NOT act as both the Pilot AtControls and Observer concwTently dming the mission. 

## Launching the Spectra flying wing
After successful completion ofthe pre-flight checklist, the Spectra should ready to perform its' mission. The most hazardous conditions for you aircraft exist during launch and landing as the aircraft is close to the ground and subject to swirling winds and unexpected circumstances. Itis advisable that the Spectra be launched by someone other than the Pilot At Controls (PAC) so that clear focus on flight ofthe Spectra canbe maintained
.. Whomever selected should have previous experience launching the trainer aircraft to ensme success. The keys to a good launch are as follows: 1. Launch directly into the wind with as much clear space in the climb out area as possible. 2. Keep the wings level as possible during launch and climb. 3. DO NOTlaunch with power on unless medical personnel are standingby. 4. Use 100% powerto initiate climb out afterthe aircraft has left the hand ofthe launcher. 5. When a good climb rate is established, reduce throttle to 80% until mission altitude is achieved. 6. In windy conditions, be ready to conect for extreme maneuvers thatcould be causedby ground turbulence. 7. Ifa collision after launch becomes imminent, reduce powerto zero as quickly as possible to reduce damage bothto the aircraft and on the ground. 

# Continued All Content & Images Copyright© RPFiightSystems, Inc. 

# "1
. .**~-!** •,

+**-~~-** -- . - - .•...,,_,....,**:~-; ~-.~..:~:--:_~~..:;.;~4"** P.O. Box 470 Wimberley, TX78676 Phone: 512.847.9746 

## Flying the Spectra wing
The Spectrahas been designed and modified over 7 years offield trials. Itis the best compromise between a rugged, robust airframe and a very stable aerial platform. The Spectra has flown and executed it's missions inenvironmental conditions that would "ground" most other small unmanned aircraft.
1. Always pre-flight your aircraft before launch. Check that all surfaces are sound andthat movement ofthe controls coincides with the appropriate stick onthe flight control transmitter. 2. Rememberthatas the aircraft flies toward you, and to correct for a bank, "the low wing gets the stick". Forexample: ifthe wing is flying toward you and from your perspective, the leftwing is down, to correct for that, youmovethe stick to the leftortowardthe "down" wing to correct and level the wing. 3. Launch sequence doesn'trequire as much control as you think. Justkeep the wings level and the aircraftwill find its own climbrate. Ifit "balloons" up too much and looks likely to stall, then slowly feed ina very small amount ofdown control. Throttle settings for normal operation are as follows: a. Launch : 100% powerfor the first 5-l0 seconds oruntil a positive climb is established. b. Sustained climb :75-80%poweruntil at altitude. c. Cruise : 50-60% power d. Slow flight/endurance : 30-40%power e. Landing : 0% power-blipthrottle as needed to control a short approach 4. ALWAYS LAUNCH DIRECTLY INTO THE WIND-NEVER ATTEMPT A DOWNWIND LAUNCH! 5. Landing sequence: The best landing sequence allows youto utilize a long, straightin approach directly into the wind. As the aircraft circles into the pattern, you canbleed offairspeed and altitude by pulling backvery slowly on the elevator stick. Ifthe throttle is off, the nose should come up, and it should slowdown significantly, and begin a gradual descent. 6. Ifyou fly your aircraft until it hits lowvoltage cutoff(LVC) you should beginyour landing sequence immediately! This "safety circuit" keeps from discharging yourbatteries to deeply. You will know when youreach LVC whenthe throttle cuts unexpectedly. This is done to conseiVe enough battery energy to power the control surfaces. You should have enoughbatterypowerto make one or two short throttle bursts to control your descent. 7. Try to flare the wing before landing to reduce forward speed asmuch as possible. Don'tpull up too soon or you will stall and it will drop quickly, possibly damaging components. 

# Continued All Content & Images Copyright © RPFlightSystems, Inc.P.O. Box470 Wimberley, TX 78676 Phone: 512.847.9746 

# Standard Video Receiver and MUX Check List.

I



# .. 

# . ·-

1. Video Patch cable 2. 2.4 Ghz video receiver 3. 8 dbi polarized patch anetnna 4. LCD Monitor Patch cable 5. LCD Video Monitor 

### The video system includes all the following items, plus the video TX and cameras in the Spectra. The wiring is straight forward The video RX is set to receive on channel 1, but can be switched to a different channel ifrequired. Take note that the video patch cable has only two RCAjacks and one mini-stereojack. The LCD monitor has 3 RCAjacks and two stereojacks. Included is a gender changer for connecting two male RCAjacks. Setup ofthe video system will be as follows: 1. Locate the video RX and insert mini stereo plug into the "AV Out"jack. 2. Plug in a 12V power source to the RX (2.5A lead acid battery) 3. Ifthe antenna is not attached, screw the type "F" connector from the antenna to the RX 4. Locate the color LCD monitor and insert the yellow mini stereo plug into the "AV In" 5. Plug in a l2V power source to the monitor (2.5A lead acid battery) 6. Plug the two male (yellow) RCAjacks into the gender changer 7. Power up the LCD monitor and check the bright/contrast wheels for adjustment. 8. Optionally, a recording device may be used in place ofthe gender changer ifthe device has both video "In" and video "Out" capabilities. 9. Before flight, be sure to tum on the video power switch on the side ofthe fuselage/pod and ensure a good signal is being received. 10. The MUX camerato camera switch is the short toggle near the shutter trigger switch. 

# Continued All Content & Images Copyright© RPFlightSystems, Inc.P.O. Box 470 Wimberley, TX78676 Phone: 512.847.9746 

# Diversity Video System and MUX CheckList.

# ;-~~~-**lllt.'lo~,\_.** I / ,.,_

### - 

# ..,

L LCD Monitor 2. Diversity video receiver 3. Hi gain polarized patch anetnna 4. LCD Patch & Power Cable 

### The video system includes all the following items, plus the video TX and cameras in the Spectra. The wiring is straight forward. The video RX is set to receive on channel 1, but can easily be switched to a different channel ifrequired. Take note that the video patch cable has only two RCAjacks and one mini-stereojack The LCD monitor has an RCAjackfor video input from the diversity video receiver. An appropriate powerplug will need to be attached to the LCD to meet your specific need. Setup ofthe video system will be as follows: 1. Locate the video diversity receiver and insert mini stereo plug into the "AV Out"jack. 2. Plug in a 12V power source to the diversity receiver 3. Your diversity receiver comes with two antenna-an omni receiver for close in operations and high gain circular polarized patch for longer ranges. 4. Ifthe antennae are not attached, screwthe type "F" connector from the antenna to the diversity. Either connector may be used. 

### S. Locate the colorLCD monitor and insert the yellow mini stereo plug into the "A V In" 6. Plug in a 12V power source to the monitor. 7. Plug the male (yel1ow) RCAjacks into the LCD connector box. 8. Power up the LCD monitor and check the bright/contrast wheels for adjustment. 9. Power up the diversity receiver by pressing the red button near thepower plug 10. Select the proper channel by pressing and releasing the power button. 11. Optionally, a recording device may be used in between the receiver and the LCD monitor. 

# Continued All Content & Images Copyright © RPFlightSystems, Inc.-------------------------------·-

P.O. Box470 Wimberley, TX 78676 Phone: 512.847.9746 

# Charger Operation
The Triton charger included inthis pack is designedto charge several differenttypes ofbatteries from a 12V power source. This power source could be a carbattery orthe 11OVAC/12VDC power supply. Mostcritical to this operation are the flight andvideo batteries. These batteries are either lithium polymer, or lithium ion invarious capacities (mah) butall produce 11.1 volts nominal. A fully charged LiOnbattery will showa voltage of 12.59 to 12.60 volts. The Triton charger is defaultedtothe correct valuesbutverify that they are correct before charging. The LCD screen should display the following :

·Battery Type :Li-On Voltage : 11.1 Charge rate is determined by the charger. These othervalues are changed by pushing onthe round spinwheel to selectthe category, thenrotating the wheel to change. 

### DO NOT CHANGE THE ll.lVVALUE TO CHARGE LITHIUM BATTERIES! Failuretoobservethisdetailcould cause a fire and explosion. 

### DO NOT CHARGE LITHIUM BATTERIES UNATTENDED either in a vehicle or structure' Use the chargerby using the following steps: I. Connectthe charger toa 12V power source. Itshould beep and startup automatically. 2. Locate the "snakehead" charging adapter and insert the bananaplugs inthe appropriately coloredjack. 3. Connectthe battery using the appropriate plug onthe charging lead. 4. Pressthe round spin wheel to initiate the charge sequence. Thevalues that canbechanged will flash butjust press the buttonto continue to the next, and the next. 5. The screen will change and the chargerwill beep-indicatingthat the charging sequence has started. 6. When the battery is topped off, the unit will automatically stop charging and emit a tone. 

# Battery Handling
Lithium batteries should never be dropped, crushed, hit, folded, spindled, fondled, kneaded, mutilated or sliced in any way shape or form. To do so invites all sorts of ill will upon your selfandyour comrades. Donot over discharge a battery ortry to charge it a higher rate than it canaccept. Iffor ANYreason a battery begins to "puffup" and get swollen, remove it to a SAFE, NON-FLAMMABLE area for observation.P.O. Box 470 Wimberley, TX78676 Phone: 512.847.9746 

# Activating the Thermal Stabilization System (optional) Missionsmay be flown successfully without the use ofthe thennal stabilization system ifso desired. The thermal stabilizationhelps damp out some ofthe effects ofwind and helps reduce the load onthe pilotby keeping the aircraft in level flight. When the system isengaged, it shouldbe notedthat themore stabilization used, the more control input is required from the ground control station to affectthe aircraft. There are some restrictions to its use, the mostcommon times NOT to use the system is : 1. During dense fog orheavy overcast 2. Over water 3. Over snow The system will advise you through offlight integrity through the calibrationprocess by activating a single control elevonfrom 1to 10 times. 1being the least amount ofintegrity, and 10 being the optimum. Tocalibrate thethermal stabilization system perform he following steps : 1. After powerup ofall systems, andjustbefore launch, point the nose ofthe aircraft straight toward the ground 2. Maintainat least 50 feet from trees, cars or nearby buildings. 3. Calibrate the unit over grass. Do not calibrate over asphaltorconcrete as heat reflected from these surfaces will causethe thermal sensorto respond inappropriately. 4. Press and hold the red "CAL"button on top ofthe cowling until one control surfaces activates. 5. Release the calibrationbuttonwhile maintaining the nose down condition. 6. The system will indicatecalibration level by activating theelevon a number oftimes. We do NOT recommend theuse ofthethennal stabilization system unless you geta returnof4 oractivations orbetter. 7. Once the calibration is complete, holdthe aircraftupright and move the right stick onthe ground control unit. You areready to launch 8. The thermal stabilization system is activated by turning the centerknob onthe face ofthe GCUto the right 9. Thedegree ofcontrol canbe "dialed in"by varyingthe centerpointoftheknob. For instance, turning the knob all the way to the right is 100% stabilization, turning the knob onlyhalfway gives 50% stabilization. 

## lO.DO NOTATTEMPf TO LAUNCHYOURAIRCRAFT WITH THE STABILIZATION SYSTEM ENGAGED! 11. Once your aircraftis at a safe altitude, activate the system and testby starting a gentle turn and releasing the sticks. The aircraft should rightit'lelf 12. The stabilization system may be used to assist inlandings. Once lined up withthe landing zone, the aircraft may allowed to land itself 13. Once the system is calibrated, it should begoodfor the duration ofthe days flying. Ifweather conditions should change drastically, thenthe unit shouldbere-calibrated.

## Appendix "B" Motion Picture and Television Operations Manual

41Page

# Q~DRONE**C~~** i 

# DYNAMICS

Motion Picture and Television Flight Operation Manual

Drone Pilot LLC PO BOX 5756 • Austin, Texas 78763 {512) 580-5100

### c.

## 1. Introduction A. Purpose

# (4~) 

# DRON:E ()
. DYNAMICS

This manual has been developed by "Drone Dynamics LLC", hereafter referred to as "Drone Dynamics", in conjunction with an exemption under Section 333 of Public Law 112-95 in reference to 49 U.S.C. 

### § 44704 for the purposes offilming. Drone Dynamic's pilots and other company personnel when applicable will comply with the policies, procedures and conditions ofthis manual, whenever motion picture ortelevision flight operations are performed that require a Waiver of Authorization as mentioned above. 

## B. Operator Organization Drone Dynamics LLC PO Box 5756 Austin, TX 78773-5756 (512) 580-51 00 office 

## C. Persons Authorized The certificate holder shall ensure that no persons are allowed within 500 feet of the area except those consenting to be involved and necessary for the filming production. This provision may be reduced to no less than 200 feet if an equivalent level of safety can be achieved and the Administrator has approved it. For example, an equivalent level of safety may be determined by an ASI's evaluation ofthe filming production area to note terrain features, obstructions, buildings, etc. Such barriers may protect nonparticipating persons (observers, the public, news media, etc.) from debris in the event of an accident. 

## D. Area of Operations Drone Dynamics' approved area of operations will be the United States.·'

## E. Plan ofActivities At leastthree (3) days prior to any scheduled filming, Drone Dynamics will submit a written plan of activities to the local FSDO having jurisdiction over that area. The plan ofactivities should include the following: (1) Dates and times for all flights (2) Name and phone number ofthe operator for the UAS aerial filming conducted underthis grant ofexemption (3) Name and phone number ofthe person responsible for the on-scene operation ofthe UAS (4) Make, model, and serial or N-Number of UAS to be used (5) Name and certificate number of UAS PICs involved in the aerial filming (6) A statement that the operator has obtained permission from property owners and/or local officials to conduct the filming production event; the list ofthose who gave permission must be made available to the inspector upon request (7) Signature of exemption holder or representative; and (8) A description ofthe flight activity, including maps or diagrams of any area, city, town, county, and/or state over which filming will be conducted and the altitudes essential to accomplish the operation. The three (3) day notification requirements may be waived, however, the operator should contact the FSDO as soon as possible with this request and be prepared to explain in detail why the three (3) day notification is not practical. 

## F. Permission to Operate All operations shall be conducted over private or controlled-access property with permission from the property owner/controller or authorized representative. Permission from property owner/controller or authorized representative will be obtained for each flight to be conducted. Persons from whom permission may be required are listed below:

### (1) 

## (2) (3) (4) (5) 

# DRON: DYNAMiCS

Property owners Law enforcement officials Fire department officials Local, State and Federal government Air traffic control Drone Dynamics personnel obtaining such permission will do so in writing whenever practical, however, verbal permission is acceptable otherwise. A standard permission form is provided in Appendix A and may be used when obtaining written permission. Drone Dynamics personnel will assure a sufficient number ofthose forms are available at the job site. Written permission forms will be maintained at thejob site until flight operations are completed, and then turned into the pilot in command 

### I flight supervisorto be kept on file for a minimum of six (6) months. These forms will be made available for inspection by the FAA or other official personnel upon request. 

## G. Security Priorto anyflight operation the operatorwill coordinate with appropriate production personnel to devise a plan of securing the area(s) of operation from all unauthorized persons and vehicles. Provisions will be made to immediately discontinue operations should the area(s) become unsecured orfor any other reason in the interest of safety. 

## H. Briefing of Pilot/Production Personnel Prior to the start ofany operation underthe provisions ofthis manual, the pilot in command will conduct a briefing ofall procedures to participating personnel ofthe risks involved, emergency procedures, and safeguards to be followed during the filming production event. Personnel will also be briefed on additional provisions that may be issued by the FSDO that has geographic responsibility for the operational area, including the location of boundaries ortime limits. The briefing shall cover: • Authorization for motion picture and television certificate ofwaiver and the

attached special provisions • Operations manual • Plan of activities

# Clf' 

# DRONE DYNAM:CS

• Radio communications • UAS activities to be conducted during the filming production event • UAS launching procedures • UAS approach and landing procedures • Recall procedures • Emergency procedures • Risks to participating personnel • How to control nonparticipating persons 

## I. Certification/Airworthiness All Drone Dynamics UAS used in operations requiring an exemption under Section 333 of Public Law 

### 112-95 in reference to 

### 49 U.S.C. 

### § 

### 44704, for the purpose offilming will be properly maintained and inspected to ensure that it is in a condition for safe operation. Prior to each flight, the PIC must conduct a pre-flight inspection and determine the UAS is in a condition for safe flight. The pre-flight inspection must account for all potential discrepancies, e.g., inoperable components, items, or equipment. Ifthe inspection reveals a condition that affects the safe operation ofthe UAS, the aircraft is prohibited from operating until the necessary maintenance has been performed and the UAS is found to be in a condition for safe flight. Drone Dynamics must follow the UAS manufacturer's maintenance, overhaul, replacement, inspection, and life limit requirements for the aircraft and aircraft components. 

## J. 

## Pilot Personnel/Minimum Requirements The pilot/operator shall establish and specify the minimum pilot requirements. Minimum requirements shall meet or exceed the following: {1) Pilot in command must hold either an airline transport, commercial, private, recreational, or sport pilot certificate. The PIC must also hold a current FAA airman medical certificate or a valid U.S. driver's license issued by a state, the District of Columbia, Puerto Rico, a territory, a possession, orthe Federal government. The PIC must also meetthe flight review requirements specified in 

### 14 CFR 

### § 

### 61.56 in an aircraft in which the PIC is rated on his or her pilot certificate.


## K. Communications

### Priorto the start of any operation covered by this manual, the pilot in command will formulate a plan to provide communications capability to all participants during the actual operation and filming. Oral, visual or radio communications may be used as long as it is effective and is capable of keeping the participants continuously appraised ofthe current status ofthe operation. 

## L. Accident Notification Should an accident or incident requiring notification ofthe NTSB occur, the notification requirements of FAR Part 

### 830 would comply. 

## M. Recall/Stop Procedures Radio communication, oral, visual or a combination will be utilized to keep the participants continuously apprised ofthe current status of operation. 

## N. Special Provisions The controls, procedures, and conditions set forth in the Drone Dynamics motion picture and television operations manual is the primary assurance that persons on the surface will not be jeopardized. The aircraft used under this authorization and/or waiver will only be those specified in attached Section 

### 333 Exemption {"Appendix B" Page 

### 15). Each pilot's name and certificate number shall appear on each daily plan of activity. All aircraft and pitot(s) participating in the activity shall be available for FAA inspection before the scheduled event. Each pilot-in-command conducting operations authorized under this certificate understands the conditions of issuance, and that it constitutes an exemption under Section 

### 333 of Public Law 

### 112-95 in reference to 

### 49 U.S.C. 

### § 44704. UAS takeoff and landing areas will be protected in a manner that will prevent unauthorized persons from entering the takeoff and landing area. Drone Dynamics will ensure that the participating persons involved in the operations are thoroughly briefed on special procedures, communication, emergency procedures, and on the provisions ofthe authorization and/or waiver before beginning the activities. No person may participate in any event unless that person has received a briefing on the provisions ofthe waiver. 

## 2. Company Organization

## A. Flight Supervisor I 

## Pilot in Command Duties and Responsibilities: • Act as liaison between Drone Dynamics and the FAA on matter concerning this manual. • Assure that each approved**pilot/oper~tor** 

### is issued a copy ofthis manual and obtain a signed statement from each that they have read and understand its contents.
• Maintain a current copy ofthis manual at the main base ofoperations for Drone Dynamics. • Responsible for assuring that all revisions to this manual are distributed and processed properly. • Assume the responsibilities of pilot in command when acting as such. • May delegate functions to other personnel but retains responsibility. 

## B. UAS Operator Duties and Responsibilities:
• Assure that aircraft to be flown is in airworthy condition and all inspections and required maintenance have been performed as per section 333 exemption.
• Acquire permission from the flight supervisor 

### I pilot in command before any operation under the provisions ofthis manual.
• Be very knowledgeable ofthe contents ofthis manual and abide by the procedures, policies and conditions contained herein.
• Coordinate with movie and television personnel to formulate plans, routes, locations, etc. with safety of all persons involved in the primary concern. • Maintain their copy ofthis manual in current condition and have it on site at anyjob or operation requiring the waiver 

## C. Payload Operator

# ~~)DRONE**~/;\** 

# DYNAMICS

Duties and Responsibilities:
• Assure that aircraft to be flown is in airworthy condition and all inspections and required maintenance have been performed as per section 333 exemption.
• Be very knowledgeable ofthe contents ofthis manual and abide by the procedures, policies and conditions contained herein.
• Maintain their copy ofthis manual in current condition and have it on site at anyjob or operation requiring the waiver.
• Coordinate with movie and television personnel to formulate shot lists.


## D. Visual Observer Duties and Responsibilities:
• Be very knowledgeable ofthe contents ofthis manual and abide by the procedures, policies and conditions contained herein.
• Maintain their copy ofthis manual in current condition and have it on site at anyjob or operation requiring the waiver.
• Maintain visual contact with the UAS while in operation and communicate with the UAS operators to ensure the safety ofall persons involved.



## Appendix A . 1

# C~~) 

# DRONE _j 

# DYNAMICS

Drone Dynamics LLC Permission Acquisition Form In signing this form, I am giving the pilots of Drone Dynamics permission to operate their aircraft at less than 500 feet from property, or in some jurisdiction in which I am responsible for or affiliated with, for the purpose offilm or television production. Name: Title: Basis ofAuthority to Grant Permission: Location: Date of Operation:
Signature ---------------------- Date

Drone Dynamics Representative Receiving Permission

# ~~JDRONE**(~)** " DYNAMICS Appendix A .2 Revision 

## Letter Rev# Section Page Action Remarks Initials

R o Remove and Replace D o Delete and Destroy N o Insert New Page 

### Manual Serial#
_________lssued To ------------

Revised 

## By

--------------- Date
This form must be returned to the Flight Supervisor no later than ----------

## Appendix B .1 ·

· (see attached Section 333 Exemption)